Linear analysis and control of a tethered system with two rigid end bodies
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference24 articles.
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1. A direct method-based suboptimal attitude guidance for accurate ground-target tracking maneuvers;Advances in Space Research;2022-06
2. Fuel-optimal deorbit scheme of space debris using tethered space-tug based on pseudospectral method;Chinese Journal of Aeronautics;2021-09
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